{
  "$type": "site.standard.document",
  "description": "A geared architecture (48) for a gas turbine engine (20) includes a lubricant manifold (76) for directing lubricant flow to the geared architecture (48). The manifold (76) including annular channel (80, 84) and a bowl member (82, 86) received within the annular channel (80, 84) for defining a…",
  "path": "/patents/1421424",
  "publishedAt": "2023-05-31T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/18",
    "RAYTHEON TECH CORP [US]"
  ],
  "textContent": "A geared architecture (48) for a gas turbine engine (20) includes a lubricant manifold (76) for directing lubricant flow to the geared architecture (48). The manifold (76) including annular channel (80, 84) and a bowl member (82, 86) received within the annular channel (80, 84) for defining a passage for directing lubricant.",
  "title": "MANIFOLD FOR GEARED TURBOFAN ENGINE"
}